CN204019184U - A kind of terminal pad frock of processing vapor turbine blade - Google Patents
A kind of terminal pad frock of processing vapor turbine blade Download PDFInfo
- Publication number
- CN204019184U CN204019184U CN201420485864.2U CN201420485864U CN204019184U CN 204019184 U CN204019184 U CN 204019184U CN 201420485864 U CN201420485864 U CN 201420485864U CN 204019184 U CN204019184 U CN 204019184U
- Authority
- CN
- China
- Prior art keywords
- cushion block
- terminal pad
- blade
- internal diameter
- frock
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn - After Issue
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Abstract
The utility model relates to a kind of terminal pad frock of processing vapor turbine blade, comprise numerical control rotary terminal pad, blade frock body, internal diameter blade is to cushion block and back edge cushion block, the side of numerical control rotary terminal pad is provided with cylindrical boss, its opposite side is point centered by the center of circle, be provided with rectangle limited block, blade frock body comprises upper and lower two parts, bottom is rectangle seat, rectangle seat and rectangle limited block matching form close, top is quadrangle die cavity, internal diameter blade is cube block structure to cushion block and back edge cushion block, internal diameter blade is close on two adjacent madial walls of quadrangle die cavity to cushion block and back edge cushion block respectively, the utility model clamped one time can complete multistep operation, not only improves operation working (machining) efficiency, ensure that each portion precision simultaneously, and can complete the unmanageable product of prior art and operation, reduces the processing cost of product, improves the economic benefit of enterprise.
Description
Technical field
The utility model belongs to field of machining, relates to blade processing technology, specifically a kind of terminal pad frock of processing vapor turbine blade.
Background technology
Along with the progress of science and technology, Machining Technology is development also, the raising of all kinds of mechanical workpieces working (machining) efficiency becomes the most eager demand of each large mechanic factory workers, but, in the process that the work in-process heart is processed workpiece, general by using frock clamp to carry out clamping fixation workpiece at present, add and then adopt vice or protractor support man-hour, clamping is repeatedly needed in process, not only inefficiency, and machining accuracy is difficult to ensure, and even some product or operation cannot complete at all, improve processing cost, adverse effect is brought to the development of manufacturing enterprise.
Utility model content
Technical problem to be solved in the utility model is, for overcoming the shortcoming of prior art, a kind of terminal pad frock of processing vapor turbine blade is provided, add man-hour, clamped one time can complete multistep operation, not only improves operation working (machining) efficiency, ensure that each portion precision simultaneously, and the unmanageable product of prior art and operation can be completed, reduce the processing cost of product, improve the economic benefit of enterprise.
In order to solve above technical problem, the utility model provides a kind of terminal pad frock of processing vapor turbine blade, comprise numerical control rotary terminal pad, blade frock body, internal diameter blade is to cushion block and back edge cushion block, the position of numerical control rotary terminal pad same circumference radius is uniformly distributed and is provided with four the first counter sinks, numerical control rotary terminal pad is circular metal plate structure, the side of numerical control rotary terminal pad is provided with cylindrical boss, its opposite side is point centered by the center of circle, be provided with rectangle limited block, rectangle limited block upper surface is arranged with two rectangular recess, article two, be arranged with two the first screwed holes in rectangular recess respectively,
Blade frock body comprises upper and lower two parts, bottom is rectangle seat, the both sides of the edge of rectangle seat bottom surface are symmetrical and be parallelly provided with two rectangular boss, the spacing of two rectangular boss is equal with the spacing of two rectangular recess, simultaneously rectangular boss and matching form corresponding with rectangular recess position closes, and four angles of rectangle seat are provided with four the second counter sinks, the second counter sink and the first screwed hole one_to_one corresponding, top is quadrangle die cavity, and both sidewalls adjacent in die cavity is provided with the second screwed hole;
Internal diameter blade is cube block structure to cushion block and back edge cushion block, and internal diameter blade is close on two adjacent madial walls of quadrangle die cavity respectively to cushion block and back edge cushion block.
The technical scheme that the utility model limits further is:
Aforementioned die cavity is parallelogram or diamond shelf structure; The diameter of cylindrical boss is 40mm.
The diameter of the cylindrical boss of numerical control rotary terminal pad reverse side is set to 40mm, matches in the hole being 40mm with the diameter of revolution four axle of numerical control machining center.
Aforementionedly be provided with on the two adjacent surfaces sidewall of the second screwed hole, wherein a sidewall is provided with second screwed hole, and another side sidewall is provided with two the second screwed holes; Internal diameter blade, on cushion block and back edge cushion block and the two adjacent surfaces sidewall be close to thereof, is respectively equipped with two through holes, and the through hole on sidewall and internal diameter blade are to the equal and position one_to_one corresponding of the hole size on cushion block and back edge cushion block.
Aforementionedly be provided with on the two adjacent surfaces sidewall of the second screwed hole, wherein a sidewall is provided with second screwed hole, and another side sidewall is provided with two the second screwed holes; Internal diameter blade, on cushion block and back edge cushion block and the two adjacent surfaces sidewall be close to thereof, is respectively equipped with two through holes, and the through hole on sidewall and internal diameter blade are to the equal and position one_to_one corresponding of the hole size on cushion block and back edge cushion block.
Four angles of blade frock body are provided with four counter sinks, it are closely connected with numerical control rotary terminal pad by four screws; And the internal diameter blade be arranged in blade frock body die cavity is to cushion block and back edge cushion block, then come by the thickness of cushion block that the center of adjusting vane is high to be consistent with the revolution axle center of four axles, blade frock body is also provided with three screwed hole screwed holes, carrys out workpiece pressing by three screws.
The beneficial effects of the utility model are:
The utility model is in process, clamped one time can complete multistep operation, improve the Product processing efficiency of machining center, make machining center can process the unmanageable product of prior art and operation in addition, meanwhile, this frock can also process multiclass workpiece simultaneously, decrease the regulation time changing workpiece, ensure that each portion precision, reduce the processing cost of product, improve the economic benefit of enterprise.
Accompanying drawing explanation
Fig. 1 is the axonometric drawing of the terminal pad frock of the utility model processing vapor turbine blade;
Fig. 2 is the front view of numerical control rotary terminal pad;
Fig. 3 is the sectional view of numerical control rotary terminal pad;
Fig. 4 is the front view of blade frock body;
Wherein, 1-numerical control rotary terminal pad, 2-blade frock body, 3-internal diameter blade to cushion block, 4-back edge cushion block.
Detailed description of the invention
embodiment 1
The present embodiment provides a kind of terminal pad frock of processing vapor turbine blade, structure is as Fig. 1, shown in Fig. 2 and Fig. 3, comprise numerical control rotary terminal pad 1, blade frock body 2, internal diameter blade is to cushion block 3 and back edge cushion block 4, the position of numerical control rotary terminal pad 1 same circumference radius is uniformly distributed and is provided with four the first counter sinks, numerical control rotary terminal pad 1 is circular metal plate structure, the side of numerical control rotary terminal pad 1 is provided with cylindrical boss, its opposite side is point centered by the center of circle, be provided with rectangle limited block, rectangle limited block upper surface is arranged with two rectangular recess, article two, be arranged with two the first screwed holes in rectangular recess respectively, blade frock body 2 comprises upper and lower two parts, bottom is rectangle seat, the both sides of the edge of rectangle seat bottom surface are symmetrical and be parallelly provided with two rectangular boss, the spacing of two rectangular boss is equal with the spacing of described two rectangular recess, simultaneously rectangular boss and matching form corresponding with rectangular recess position closes, four angles of rectangle seat are provided with four the second counter sinks, second counter sink and the first screwed hole one_to_one corresponding, top is quadrangle die cavity, and both sidewalls adjacent in die cavity is provided with the second screwed hole, internal diameter blade is cube block structure to cushion block 3 and back edge cushion block 4, and internal diameter blade is close on two adjacent madial walls of quadrangle die cavity respectively to cushion block 3 and back edge cushion block 4.
Aforementioned die cavity is parallelogram lever structure, and the diameter of cylindrical boss is 40mm.
As shown in Figure 4, be aforementionedly provided with on the two adjacent surfaces sidewall of the second screwed hole, wherein a sidewall is provided with second screwed hole, and another side sidewall is provided with two the second screwed holes; Internal diameter blade, on cushion block 3 and back edge cushion block 4 and the two adjacent surfaces sidewall be close to thereof, is respectively equipped with two through holes, and the through hole on sidewall and internal diameter blade are to the equal and position one_to_one corresponding of the hole size on cushion block 3 and back edge cushion block 4.
During use, screw is used to be arranged on numerical control rotary terminal pad 1 by blade frock body 2, again the cylindrical boss of numerical control rotary terminal pad 1 reverse side is aimed at the borehole jack jail of revolution four axle, bolt is adopted to be arranged on revolution four axle of numerical control machining center by the first counter sink by numerical control rotary terminal pad 1, then internal diameter blade is set in the die cavity of blade frock body to cushion block and back edge cushion block, the center being carried out adjusting vane by the cushion block changing different-thickness is high, until the revolution axle center of itself and four axles is consistent, screwed hole place mounting screw simultaneously on blade frock body sidewall carrys out workpiece pressing, can process workpiece.
Above embodiment is only and technological thought of the present utility model is described; protection domain of the present utility model can not be limited with this; every technological thought according to the utility model proposes, any change that technical scheme basis is done, all falls within the utility model protection domain.
Claims (5)
1. the terminal pad frock of a processing vapor turbine blade, comprise numerical control rotary terminal pad (1), blade frock body (2), internal diameter blade is to cushion block (3) and back edge cushion block (4), the position of numerical control rotary terminal pad (1) same circumference radius is uniformly distributed and is provided with four the first counter sinks, it is characterized in that, described numerical control rotary terminal pad (1) is circular metal plate structure, the side of described numerical control rotary terminal pad (1) is provided with cylindrical boss, its opposite side is point centered by the center of circle, be provided with rectangle limited block, described rectangle limited block upper surface is arranged with two rectangular recess, article two, be arranged with two the first screwed holes in described rectangular recess respectively,
Described blade frock body (2) comprises upper and lower two parts, described bottom is rectangle seat, the both sides of the edge of described rectangle seat bottom surface are symmetrical and be parallelly provided with two rectangular boss, the spacing of described two rectangular boss is equal with the spacing of described two rectangular recess, simultaneously described rectangular boss and matching form corresponding with described rectangular recess position closes, four angles of described rectangle seat are provided with four the second counter sinks, described second counter sink and described first screwed hole one_to_one corresponding, described top is quadrangle die cavity, both sidewalls adjacent in described die cavity is provided with the second screwed hole,
Described internal diameter blade is cube block structure to cushion block (3) and back edge cushion block (4), and described internal diameter blade is close on two adjacent madial walls of described quadrangle die cavity respectively to cushion block (3) and back edge cushion block (4).
2. the terminal pad frock of processing vapor turbine blade according to claim 1, is characterized in that, described die cavity is parallelogram or diamond shelf structure.
3. the terminal pad frock of processing vapor turbine blade according to claim 1, is characterized in that, the diameter of described cylindrical boss is 40mm.
4. the terminal pad frock of processing vapor turbine blade according to claim 1, is characterized in that, described in be provided with on the two adjacent surfaces sidewall of the second screwed hole, wherein a sidewall is provided with second screwed hole, and another side sidewall is provided with two the second screwed holes.
5. the terminal pad frock of processing vapor turbine blade according to claim 1, it is characterized in that, described internal diameter blade is on cushion block (3) and back edge cushion block (4) and the two adjacent surfaces sidewall be close to thereof, be respectively equipped with two through holes, the through hole on described sidewall and described internal diameter blade are to the equal and position one_to_one corresponding of the hole size on cushion block (3) and back edge cushion block (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420485864.2U CN204019184U (en) | 2014-08-26 | 2014-08-26 | A kind of terminal pad frock of processing vapor turbine blade |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420485864.2U CN204019184U (en) | 2014-08-26 | 2014-08-26 | A kind of terminal pad frock of processing vapor turbine blade |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204019184U true CN204019184U (en) | 2014-12-17 |
Family
ID=52059092
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420485864.2U Withdrawn - After Issue CN204019184U (en) | 2014-08-26 | 2014-08-26 | A kind of terminal pad frock of processing vapor turbine blade |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204019184U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104191269A (en) * | 2014-08-26 | 2014-12-10 | 南京赛达机械制造有限公司 | Connecting disc tool for machining turbine blade |
-
2014
- 2014-08-26 CN CN201420485864.2U patent/CN204019184U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104191269A (en) * | 2014-08-26 | 2014-12-10 | 南京赛达机械制造有限公司 | Connecting disc tool for machining turbine blade |
| CN104191269B (en) * | 2014-08-26 | 2016-05-04 | 南京赛达机械制造有限公司 | A kind of terminal pad frock of processing vapor turbine blade |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20141217 Effective date of abandoning: 20160504 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |